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pro vyhledávání: '"K. L. Suder"'
Publikováno v:
Journal of Turbomachinery. 121:517-524
This paper presents the first attempt to stabilize rotating stall in a single-stage transonic axial flow compressor with inlet distortion using active feedback control. The experiments were conducted at the NASA Lewis Research Center on a single-stag
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5bfce7e041152dbc991de11b001b60b0
https://doi.org/10.1115/1.2841346
https://doi.org/10.1115/1.2841346
Publikováno v:
Journal of Turbomachinery. 121:510-516
This paper presents the first attempt to stabilize rotating stall in a single-stage transonic axial flow compressor with inlet distortion using active feedback control. The experiments were conducted at the NASA Lewis Research Center on a single-stag
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e832983a3768be38f2671a5bcb74e164
https://doi.org/10.1115/1.2841345
https://doi.org/10.1115/1.2841345
Autor:
K. L. Suder
Publikováno v:
Journal of Turbomachinery. 120:465-476
A detailed experimental investigation to understand and quantify the development of blockage in the flow field of a transonic, axial flow compressor rotor (NASA Rotor 37) has been undertaken. Detailed laser anemometer measurements were acquired upstr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd94a513aa014ae3bdf4cdbf28f0c166
https://doi.org/10.1115/1.2841741
https://doi.org/10.1115/1.2841741